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FR3087419B1 - AIRCRAFT ENGINE NACELLE INCLUDING AN ICE PROTECTION SYSTEM. - Google Patents

AIRCRAFT ENGINE NACELLE INCLUDING AN ICE PROTECTION SYSTEM. Download PDF

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Publication number
FR3087419B1
FR3087419B1 FR1871236A FR1871236A FR3087419B1 FR 3087419 B1 FR3087419 B1 FR 3087419B1 FR 1871236 A FR1871236 A FR 1871236A FR 1871236 A FR1871236 A FR 1871236A FR 3087419 B1 FR3087419 B1 FR 3087419B1
Authority
FR
France
Prior art keywords
protection system
aircraft engine
engine nacelle
ice protection
nacelle
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1871236A
Other languages
French (fr)
Other versions
FR3087419A1 (en
Inventor
Alain Porte
Francois Pons
Gregory Albet
Maxime Zebian
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1871236A priority Critical patent/FR3087419B1/en
Priority to EP19203144.1A priority patent/EP3640140A1/en
Priority to CN201910988180.1A priority patent/CN111071461A/en
Priority to US16/655,406 priority patent/US11643216B2/en
Publication of FR3087419A1 publication Critical patent/FR3087419A1/en
Application granted granted Critical
Publication of FR3087419B1 publication Critical patent/FR3087419B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02—De-icing means for engines having icing phenomena
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Other Air-Conditioning Systems (AREA)

Abstract

Nacelle de moteur d'aéronef comprenant un système de protection contre le givre. Le système de protection (1) contre le givre pour nacelle (2) de moteur (3) d'aéronef, la nacelle (2) comprenant une virole interne (5), une lèvre (7) d'entrée d'air formant un bord d'attaque de la nacelle (2), le système de protection comprenant un dispositif échangeur de chaleur (11) comportant au moins un caloduc (12) configuré pour transférer à la virole interne (5) de la chaleur (14) émise par une source chaude.Aircraft engine nacelle comprising an ice protection system. The protection system (1) against frost for an aircraft engine nacelle (2) (3), the nacelle (2) comprising an internal ferrule (5), an air inlet lip (7) forming a leading edge of the nacelle (2), the protection system comprising a heat exchanger device (11) comprising at least one heat pipe (12) configured to transfer to the internal shell (5) heat (14) emitted by a hot spring.

FR1871236A 2018-10-19 2018-10-19 AIRCRAFT ENGINE NACELLE INCLUDING AN ICE PROTECTION SYSTEM. Active FR3087419B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1871236A FR3087419B1 (en) 2018-10-19 2018-10-19 AIRCRAFT ENGINE NACELLE INCLUDING AN ICE PROTECTION SYSTEM.
EP19203144.1A EP3640140A1 (en) 2018-10-19 2019-10-15 Aircraft engine nacelle comprising an ice protection system
CN201910988180.1A CN111071461A (en) 2018-10-19 2019-10-17 Nacelle of an aircraft engine comprising an anti-icing protection system
US16/655,406 US11643216B2 (en) 2018-10-19 2019-10-17 Aircraft engine nacelle comprising a system of ice protection

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1871236A FR3087419B1 (en) 2018-10-19 2018-10-19 AIRCRAFT ENGINE NACELLE INCLUDING AN ICE PROTECTION SYSTEM.

Publications (2)

Publication Number Publication Date
FR3087419A1 FR3087419A1 (en) 2020-04-24
FR3087419B1 true FR3087419B1 (en) 2020-10-30

Family

ID=65444233

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1871236A Active FR3087419B1 (en) 2018-10-19 2018-10-19 AIRCRAFT ENGINE NACELLE INCLUDING AN ICE PROTECTION SYSTEM.

Country Status (4)

Country Link
US (1) US11643216B2 (en)
EP (1) EP3640140A1 (en)
CN (1) CN111071461A (en)
FR (1) FR3087419B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3070674B1 (en) * 2017-09-06 2019-09-13 Safran Nacelles INTEGRATION WITH ACOUSTIC LEVER DEGIVREE
FR3120352B1 (en) 2021-03-03 2024-03-08 Airbus Operations Sas NACELLE AIR INLET EQUIPPED WITH A MIXED ICE PROTECTION SYSTEM
CN112977836B (en) * 2021-05-11 2021-08-10 中国空气动力研究与发展中心低速空气动力研究所 Anti-icing device

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7823374B2 (en) 2006-08-31 2010-11-02 General Electric Company Heat transfer system and method for turbine engine using heat pipes
US8015788B2 (en) * 2006-12-27 2011-09-13 General Electric Company Heat transfer system for turbine engine using heat pipes
EP2318683A2 (en) * 2008-07-30 2011-05-11 Aircelle Acoustic attenuation panel for aircraft engine nacelle
EP2391542B1 (en) 2009-02-02 2014-07-30 Airbus Operations (S.A.S.) Engine nacelle having a noise reducing structure
GB2470043B (en) 2009-05-06 2011-06-08 Gkn Aerospace Services Ltd Heating system
FR2976557B1 (en) * 2011-06-20 2013-07-12 Airbus Operations Sas METHOD FOR MAKING A PANEL FOR ACOUSTIC TREATMENT INCORPORATING THE FUNCTION OF TREATING FROZEN WITH HOT AIR
FR2976709B1 (en) * 2011-06-20 2013-07-12 Airbus Operations Sas METHOD FOR PRODUCING A PANEL FOR ACOUSTIC PROCESSING INTEGRATING CHANNELS JUXTAPOSES WITH A ALVEOLAR STRUCTURE
FR2980774B1 (en) * 2011-10-03 2013-10-25 Airbus Operations Sas AIRCRAFT NACELLE COMPRISING A HOT AIR SUPPLY DEVICE OF A PANEL COMBINING ACOUSTIC AND FROZEN TREATMENTS
FR2981049B1 (en) * 2011-10-07 2014-04-11 Aircelle Sa METHOD FOR MANUFACTURING AN ACOUSTIC ABSORPTION PANEL
EP2994618B1 (en) * 2013-05-07 2017-03-01 General Electric Company Anti-ice splitter nose
US9950799B2 (en) * 2016-03-09 2018-04-24 Honeywell International Inc. Shielded anti-icing system and methods
FR3072649B1 (en) * 2017-10-20 2019-11-08 Airbus Operations SPRAY PROTECTION SYSTEM FOR AN AIRCRAFT ENGINE NACELLE
FR3077268A1 (en) * 2018-01-26 2019-08-02 Airbus Operations DEVICE FOR DEFROSTING A CONFIGURED SURFACE TO NOT GENERATE ELECTROMAGNETIC INTERFERENCE
FR3087420B1 (en) * 2018-10-19 2021-03-12 Airbus Operations Sas AIRCRAFT ENGINE NACELLE INCLUDING AN ICE PROTECTION SYSTEM.

Also Published As

Publication number Publication date
FR3087419A1 (en) 2020-04-24
US20200122844A1 (en) 2020-04-23
US11643216B2 (en) 2023-05-09
CN111071461A (en) 2020-04-28
EP3640140A1 (en) 2020-04-22

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